Light
Dark
System
Log In
Loading...
Compare / EASA/
Incorporated Amendments
/
Compare & Highlight Differences
AMC5 CAT.IDE.A.190 Flight data recorder
Available versions for ERULES-1963177438-12649
ED Decision 2015/007/R
found in: Air Operations (965/2012) Part-ARO Part-ORO Part-CAT Part-SPA Part-NCC Part-NCO Part-SPO (Feb 2025)
From
Air Operations Rev... (Mar 2026)
Air Operations (96... (Feb 2025)
Air Operations (96... (Sep 2023)
From section
To
Air Operations Rev... (Mar 2026)
Air Operations (96... (Feb 2025)
Air Operations (96... (Sep 2023)
To section
No visible text changes
0 removals
0 additions
View
Rich
Plain
Sync scrolling
Share
From
Show details
Hide details
To
Show details
Hide details
Version
Show side by side
AMC5 CAT.IDE.A.190 Flight data recorder ED Decision 2015/007/R PERFORMANCE SPECIFICATIONS FOR THE PARAMETERS TO BE RECORDED FOR AEROPLANES FIRST ISSUED WITH AN INDIVIDUAL COFA UP TO AND INCLUDING 31 MARCH 1998 Table 1: Flight data recorder <table border="1" cellpadding="0" cellspacing="0" width="100%"><thead><tr><td width="3%"><p align="center">No</p></td><td width="17%"><p align="center">Parameter</p></td><td width="14%"><p align="center">Range</p></td><td width="8%"><p align="center">Sampling interval in seconds</p></td><td width="15%"><p align="center">Accuracy limits (sensor input compared to FDR readout)</p></td><td width="10%"><p align="center">Recommended resolution in readout</p></td><td width="29%"><p align="center">Remarks</p></td></tr></thead><tr><td valign="top" width="3%"><p>1</p></td><td valign="top" width="17%"><p>Time or relative time count</p></td><td valign="top" width="14%"><p>24 hours</p></td><td valign="top" width="8%"><p>4</p></td><td valign="top" width="15%"><p>±0.125 % per hour</p></td><td valign="top" width="10%"><p>1 second</p></td><td valign="top" width="29%"><p>Coordinated universal time (UTC) preferred where available, otherwise elapsed time</p></td></tr><tr><td valign="top" width="3%"><p>2</p></td><td valign="top" width="17%"><p>Pressure altitude</p></td><td valign="top" width="14%"><p>-1 000 ft to maximum certificated altitude of aircraft +5 000 ft</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>±100 ft to ±700 ft</p></td><td valign="top" width="10%"><p>5 ft</p></td><td valign="top" width="29%"><p>For altitude record error see EASA ETSO-C124a</p></td></tr><tr><td valign="top" width="3%"><p>3</p></td><td valign="top" width="17%"><p>Indicated airspeed or calibrated airspeed</p></td><td valign="top" width="14%"><p>50 kt to max V<sub>S0</sub></p><p>Max V<sub>S0 </sub>to 1.2 V<sub>D</sub></p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>±5 %</p><p>±3 %</p></td><td valign="top" width="10%"><p>1 kt</p></td><td valign="top" width="29%"><p>V<sub>S0</sub> stalling speed or minimum steady flight speed in the landing configuration V<sub>D </sub>design diving speed</p></td></tr><tr><td valign="top" width="3%"><p>4</p></td><td valign="top" width="17%"><p>Heading</p></td><td valign="top" width="14%"><p>360 degrees</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>±2 degrees</p></td><td valign="top" width="10%"><p>0.5 degrees</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>5</p></td><td valign="top" width="17%"><p>Normal acceleration</p></td><td valign="top" width="14%"><p>-3 g to +6 g</p></td><td valign="top" width="8%"><p>0.125 ±</p></td><td valign="top" width="15%"><p>±1 % of maximum range excluding a datum error of ±5 %</p></td><td valign="top" width="10%"><p>0.004 g</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>6</p></td><td valign="top" width="17%"><p>Pitch attitude</p></td><td valign="top" width="14%"><p>±75 degrees</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>±2 degrees</p></td><td valign="top" width="10%"><p>0.5 degrees</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>7</p></td><td valign="top" width="17%"><p>Roll attitude</p></td><td valign="top" width="14%"><p>±180 degrees </p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>±2 degrees </p></td><td valign="top" width="10%"><p>0.5 degrees</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>8</p></td><td valign="top" width="17%"><p>Manual radio transmission keying</p></td><td valign="top" width="14%"><p>Discrete</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>-</p></td><td valign="top" width="10%"><p>-</p></td><td valign="top" width="29%"><p>On-off (one discrete). An FDR/CVR time synchronisation signal complying with 4.2.1 of EUROCAE ED-55 is considered to be an acceptable alternative means of compliance.</p></td></tr><tr><td valign="top" width="3%"><p>9</p></td><td valign="top" width="17%"><p>Power on each engine</p></td><td valign="top" width="14%"><p>Full range</p></td><td valign="top" width="8%"><p>Each engine each second</p></td><td valign="top" width="15%"><p>±2 %</p></td><td valign="top" width="10%"><p>0.2 % of full range</p></td><td valign="top" width="29%"><p>Sufficient parameters e.g. EPR/N, or Torque/N<sub>P</sub> as appropriate to the particular engine should be recorded to determine power.</p></td></tr><tr><td valign="top" width="3%"><p>10</p></td><td valign="top" width="17%"><p>Trailing edge flap or flight crew compartment control selection</p></td><td valign="top" width="14%"><p>Full range or each discrete position</p></td><td valign="top" width="8%"><p>2</p></td><td valign="top" width="15%"><p>±5 % or as pilot’s indicator</p></td><td valign="top" width="10%"><p>0.5 % of full range</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>11</p></td><td valign="top" width="17%"><p>Leading edge flap or flight crew compartment control selection</p></td><td valign="top" width="14%"><p>Full range or each discrete position</p></td><td valign="top" width="8%"><p>2</p></td><td valign="top" width="15%"><p>-</p></td><td valign="top" width="10%"><p>0.5 % of full range</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>12</p></td><td valign="top" width="17%"><p>Thrust reverser position</p></td><td valign="top" width="14%"><p>Stowed, in transit and reverse</p></td><td valign="top" width="8%"><p>Each reverser each second</p></td><td valign="top" width="15%"><p>±2 % unless higher accuracy uniquely required</p></td><td valign="top" width="10%"><p>-</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>13</p></td><td valign="top" width="17%"><p>Ground spoiler and/or speed brake selection</p></td><td valign="top" width="14%"><p>Full range or each discrete position</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>±2 degrees</p></td><td valign="top" width="10%"><p>0.2 % of full range</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>14</p></td><td valign="top" width="17%"><p>Outside air temperatures or total air temperature</p></td><td valign="top" width="14%"><p>Sensor range</p></td><td valign="top" width="8%"><p>2</p></td><td valign="top" width="15%"><p>-</p></td><td valign="top" width="10%"><p>0.3ºC</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>15a</p><p>15b</p></td><td valign="top" width="17%"><p>Autopilot engagement status</p><p>Autopilot operating modes, auto-throttle and AFCS systems engagement status and operating modes</p></td><td valign="top" width="14%"><p><br/><br/></p><p>A suitable combination of discretes</p></td><td valign="top" width="8%"><p><br/><br/></p><p>1</p></td><td valign="top" width="15%"></td><td valign="top" width="10%"><p><br/><br/></p><p>-</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>16</p></td><td valign="top" width="17%"><p>Longitudinal acceleration</p></td><td valign="top" width="14%"><p>± 1 g</p></td><td valign="top" width="8%"><p>0.25</p></td><td valign="top" width="15%"><p>±1.5 % of maximum range excluding a datum error of ±5 %</p></td><td valign="top" width="10%"><p>0.004 g</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>17</p></td><td valign="top" width="17%"><p>Lateral acceleration</p></td><td valign="top" width="14%"><p>±1 g</p></td><td valign="top" width="8%"><p>0.25</p></td><td valign="top" width="15%"><p>±1.5 % of maximum range excluding a datum error of ±5 %</p></td><td valign="top" width="10%"><p>0.004 g</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>18</p></td><td valign="top" width="17%"><p>Primary flight controls, control surface positions and/or pilot input (pitch, roll, yaw)</p></td><td valign="top" width="14%"><p>Full range</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>±2 degrees unless higher accuracy uniquely required</p></td><td valign="top" width="10%"><p>0.2 % of full range</p></td><td valign="top" width="29%"><p>For aeroplanes with conventional control systems, ‘or’ applies.</p><p>For aeroplanes with non-mechanical control systems, ‘and’ applies.</p><p>For aeroplanes with split surfaces, a suitable combination of inputs is acceptable in lieu of recording each surface separately.</p></td></tr><tr><td valign="top" width="3%"><p>19</p></td><td valign="top" width="17%"><p>Pitch trim position</p></td><td valign="top" width="14%"><p>Full range</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>±3 % unless higher accuracy uniquely required</p></td><td valign="top" width="10%"><p>0.3 % of full range</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>20</p></td><td valign="top" width="17%"><p>Radio altitude</p></td><td valign="top" width="14%"><p>-20 ft to +2 500 ft</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>±2 ft or ±3 % whichever is greater below 500 ft and ±5 % above 500 ft</p></td><td valign="top" width="10%"><p>1 ft below 500 ft, 1 ft +5 % of full range above 500 ft</p></td><td valign="top" width="29%"><p>As installed. Accuracy limits are recommended</p></td></tr><tr><td valign="top" width="3%"><p>21</p></td><td valign="top" width="17%"><p>Glide path deviation</p></td><td valign="top" width="14%"><p>Signal range</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>±3 %</p></td><td valign="top" width="10%"><p>0.3 % of full range</p></td><td valign="top" width="29%"><p>As installed. Accuracy limits are recommended</p></td></tr><tr><td valign="top" width="3%"><p>22</p></td><td valign="top" width="17%"><p>Localiser deviation</p></td><td valign="top" width="14%"><p>Signal range</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>±3 %</p></td><td valign="top" width="10%"><p>0.3 % of full range</p></td><td valign="top" width="29%"><p>As installed. Accuracy limits are recommended.</p></td></tr><tr><td valign="top" width="3%"><p>23</p></td><td valign="top" width="17%"><p>Marker beacon passage</p></td><td valign="top" width="14%"><p>Discrete</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>–</p></td><td valign="top" width="10%"><p>–</p></td><td valign="top" width="29%"><p>A single discrete is acceptable for all markers.</p></td></tr><tr><td valign="top" width="3%"><p>24</p></td><td valign="top" width="17%"><p>Master warning</p></td><td valign="top" width="14%"><p>Discrete</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>–</p></td><td valign="top" width="10%"><p>–</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>25</p></td><td valign="top" width="17%"><p>NAV 1 and 2 frequency selection</p></td><td valign="top" width="14%"><p>Full range</p></td><td valign="top" width="8%"><p>4</p></td><td valign="top" width="15%"><p>As installed</p></td><td valign="top" width="10%"><p>–</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>26</p></td><td valign="top" width="17%"><p>DME 1 and 2 distance</p></td><td valign="top" width="14%"><p>0-200 NM</p></td><td valign="top" width="8%"><p>4</p></td><td valign="top" width="15%"><p>As installed</p></td><td valign="top" width="10%"><p>–</p></td><td valign="top" width="29%"><p>Recording of latitude and longitude from INS or other navigation system is a preferred alternative.</p></td></tr><tr><td valign="top" width="3%"><p>27</p></td><td valign="top" width="17%"><p>Landing gear squat switch status</p></td><td valign="top" width="14%"><p>Discrete</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>–</p></td><td valign="top" width="10%"><p>–</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>28</p></td><td valign="top" width="17%"><p>Ground proximity warning system (GPWS)</p></td><td valign="top" width="14%"><p>Discrete</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>–</p></td><td valign="top" width="10%"><p>–</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>29</p></td><td valign="top" width="17%"><p>Angle of attack</p></td><td valign="top" width="14%"><p>Full range</p></td><td valign="top" width="8%"><p>0.5</p></td><td valign="top" width="15%"><p>As installed</p></td><td valign="top" width="10%"><p>0.3 % of full range</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>30</p></td><td valign="top" width="17%"><p>Hydraulics</p></td><td valign="top" width="14%"><p>Discrete(s)</p></td><td valign="top" width="8%"><p>2</p></td><td valign="top" width="15%"><p>–</p></td><td valign="top" width="10%"><p>–</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>31</p></td><td valign="top" width="17%"><p>Navigation data</p></td><td valign="top" width="14%"><p>As installed</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>As installed</p></td><td valign="top" width="10%"><p>–</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>32</p></td><td valign="top" width="17%"><p>Landing gear or gear selector position</p></td><td valign="top" width="14%"><p>Discrete</p></td><td valign="top" width="8%"><p>4</p></td><td valign="top" width="15%"><p>As installed</p></td><td valign="top" width="10%"><p>–</p></td><td valign="top" width="29%"></td></tr></table> \* The number in the left hand column reflects the serial number depicted in EUROCAE Document ED-112.
AMC5 CAT.IDE.A.190 Flight data recorder ED Decision 2015/007/R PERFORMANCE SPECIFICATIONS FOR THE PARAMETERS TO BE RECORDED FOR AEROPLANES FIRST ISSUED WITH AN INDIVIDUAL COFA UP TO AND INCLUDING 31 MARCH 1998 Table 1: Flight data recorder <table border="1" cellpadding="0" cellspacing="0" width="100%"><thead><tr><td width="3%"><p align="center">No</p></td><td width="17%"><p align="center">Parameter</p></td><td width="14%"><p align="center">Range</p></td><td width="8%"><p align="center">Sampling interval in seconds</p></td><td width="15%"><p align="center">Accuracy limits (sensor input compared to FDR readout)</p></td><td width="10%"><p align="center">Recommended resolution in readout</p></td><td width="29%"><p align="center">Remarks</p></td></tr></thead><tr><td valign="top" width="3%"><p>1</p></td><td valign="top" width="17%"><p>Time or relative time count</p></td><td valign="top" width="14%"><p>24 hours</p></td><td valign="top" width="8%"><p>4</p></td><td valign="top" width="15%"><p>±0.125 % per hour</p></td><td valign="top" width="10%"><p>1 second</p></td><td valign="top" width="29%"><p>Coordinated universal time (UTC) preferred where available, otherwise elapsed time</p></td></tr><tr><td valign="top" width="3%"><p>2</p></td><td valign="top" width="17%"><p>Pressure altitude</p></td><td valign="top" width="14%"><p>-1 000 ft to maximum certificated altitude of aircraft +5 000 ft</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>±100 ft to ±700 ft</p></td><td valign="top" width="10%"><p>5 ft</p></td><td valign="top" width="29%"><p>For altitude record error see EASA ETSO-C124a</p></td></tr><tr><td valign="top" width="3%"><p>3</p></td><td valign="top" width="17%"><p>Indicated airspeed or calibrated airspeed</p></td><td valign="top" width="14%"><p>50 kt to max V<sub>S0</sub></p><p>Max V<sub>S0 </sub>to 1.2 V<sub>D</sub></p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>±5 %</p><p>±3 %</p></td><td valign="top" width="10%"><p>1 kt</p></td><td valign="top" width="29%"><p>V<sub>S0</sub> stalling speed or minimum steady flight speed in the landing configuration V<sub>D </sub>design diving speed</p></td></tr><tr><td valign="top" width="3%"><p>4</p></td><td valign="top" width="17%"><p>Heading</p></td><td valign="top" width="14%"><p>360 degrees</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>±2 degrees</p></td><td valign="top" width="10%"><p>0.5 degrees</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>5</p></td><td valign="top" width="17%"><p>Normal acceleration</p></td><td valign="top" width="14%"><p>-3 g to +6 g</p></td><td valign="top" width="8%"><p>0.125 ±</p></td><td valign="top" width="15%"><p>±1 % of maximum range excluding a datum error of ±5 %</p></td><td valign="top" width="10%"><p>0.004 g</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>6</p></td><td valign="top" width="17%"><p>Pitch attitude</p></td><td valign="top" width="14%"><p>±75 degrees</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>±2 degrees</p></td><td valign="top" width="10%"><p>0.5 degrees</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>7</p></td><td valign="top" width="17%"><p>Roll attitude</p></td><td valign="top" width="14%"><p>±180 degrees </p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>±2 degrees </p></td><td valign="top" width="10%"><p>0.5 degrees</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>8</p></td><td valign="top" width="17%"><p>Manual radio transmission keying</p></td><td valign="top" width="14%"><p>Discrete</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>-</p></td><td valign="top" width="10%"><p>-</p></td><td valign="top" width="29%"><p>On-off (one discrete). An FDR/CVR time synchronisation signal complying with 4.2.1 of EUROCAE ED-55 is considered to be an acceptable alternative means of compliance.</p></td></tr><tr><td valign="top" width="3%"><p>9</p></td><td valign="top" width="17%"><p>Power on each engine</p></td><td valign="top" width="14%"><p>Full range</p></td><td valign="top" width="8%"><p>Each engine each second</p></td><td valign="top" width="15%"><p>±2 %</p></td><td valign="top" width="10%"><p>0.2 % of full range</p></td><td valign="top" width="29%"><p>Sufficient parameters e.g. EPR/N, or Torque/N<sub>P</sub> as appropriate to the particular engine should be recorded to determine power.</p></td></tr><tr><td valign="top" width="3%"><p>10</p></td><td valign="top" width="17%"><p>Trailing edge flap or flight crew compartment control selection</p></td><td valign="top" width="14%"><p>Full range or each discrete position</p></td><td valign="top" width="8%"><p>2</p></td><td valign="top" width="15%"><p>±5 % or as pilot’s indicator</p></td><td valign="top" width="10%"><p>0.5 % of full range</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>11</p></td><td valign="top" width="17%"><p>Leading edge flap or flight crew compartment control selection</p></td><td valign="top" width="14%"><p>Full range or each discrete position</p></td><td valign="top" width="8%"><p>2</p></td><td valign="top" width="15%"><p>-</p></td><td valign="top" width="10%"><p>0.5 % of full range</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>12</p></td><td valign="top" width="17%"><p>Thrust reverser position</p></td><td valign="top" width="14%"><p>Stowed, in transit and reverse</p></td><td valign="top" width="8%"><p>Each reverser each second</p></td><td valign="top" width="15%"><p>±2 % unless higher accuracy uniquely required</p></td><td valign="top" width="10%"><p>-</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>13</p></td><td valign="top" width="17%"><p>Ground spoiler and/or speed brake selection</p></td><td valign="top" width="14%"><p>Full range or each discrete position</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>±2 degrees</p></td><td valign="top" width="10%"><p>0.2 % of full range</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>14</p></td><td valign="top" width="17%"><p>Outside air temperatures or total air temperature</p></td><td valign="top" width="14%"><p>Sensor range</p></td><td valign="top" width="8%"><p>2</p></td><td valign="top" width="15%"><p>-</p></td><td valign="top" width="10%"><p>0.3ºC</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>15a</p><p>15b</p></td><td valign="top" width="17%"><p>Autopilot engagement status</p><p>Autopilot operating modes, auto-throttle and AFCS systems engagement status and operating modes</p></td><td valign="top" width="14%"><p><br/><br/></p><p>A suitable combination of discretes</p></td><td valign="top" width="8%"><p><br/><br/></p><p>1</p></td><td valign="top" width="15%"></td><td valign="top" width="10%"><p><br/><br/></p><p>-</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>16</p></td><td valign="top" width="17%"><p>Longitudinal acceleration</p></td><td valign="top" width="14%"><p>± 1 g</p></td><td valign="top" width="8%"><p>0.25</p></td><td valign="top" width="15%"><p>±1.5 % of maximum range excluding a datum error of ±5 %</p></td><td valign="top" width="10%"><p>0.004 g</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>17</p></td><td valign="top" width="17%"><p>Lateral acceleration</p></td><td valign="top" width="14%"><p>±1 g</p></td><td valign="top" width="8%"><p>0.25</p></td><td valign="top" width="15%"><p>±1.5 % of maximum range excluding a datum error of ±5 %</p></td><td valign="top" width="10%"><p>0.004 g</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>18</p></td><td valign="top" width="17%"><p>Primary flight controls, control surface positions and/or pilot input (pitch, roll, yaw)</p></td><td valign="top" width="14%"><p>Full range</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>±2 degrees unless higher accuracy uniquely required</p></td><td valign="top" width="10%"><p>0.2 % of full range</p></td><td valign="top" width="29%"><p>For aeroplanes with conventional control systems, ‘or’ applies.</p><p>For aeroplanes with non-mechanical control systems, ‘and’ applies.</p><p>For aeroplanes with split surfaces, a suitable combination of inputs is acceptable in lieu of recording each surface separately.</p></td></tr><tr><td valign="top" width="3%"><p>19</p></td><td valign="top" width="17%"><p>Pitch trim position</p></td><td valign="top" width="14%"><p>Full range</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>±3 % unless higher accuracy uniquely required</p></td><td valign="top" width="10%"><p>0.3 % of full range</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>20</p></td><td valign="top" width="17%"><p>Radio altitude</p></td><td valign="top" width="14%"><p>-20 ft to +2 500 ft</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>±2 ft or ±3 % whichever is greater below 500 ft and ±5 % above 500 ft</p></td><td valign="top" width="10%"><p>1 ft below 500 ft, 1 ft +5 % of full range above 500 ft</p></td><td valign="top" width="29%"><p>As installed. Accuracy limits are recommended</p></td></tr><tr><td valign="top" width="3%"><p>21</p></td><td valign="top" width="17%"><p>Glide path deviation</p></td><td valign="top" width="14%"><p>Signal range</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>±3 %</p></td><td valign="top" width="10%"><p>0.3 % of full range</p></td><td valign="top" width="29%"><p>As installed. Accuracy limits are recommended</p></td></tr><tr><td valign="top" width="3%"><p>22</p></td><td valign="top" width="17%"><p>Localiser deviation</p></td><td valign="top" width="14%"><p>Signal range</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>±3 %</p></td><td valign="top" width="10%"><p>0.3 % of full range</p></td><td valign="top" width="29%"><p>As installed. Accuracy limits are recommended.</p></td></tr><tr><td valign="top" width="3%"><p>23</p></td><td valign="top" width="17%"><p>Marker beacon passage</p></td><td valign="top" width="14%"><p>Discrete</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>–</p></td><td valign="top" width="10%"><p>–</p></td><td valign="top" width="29%"><p>A single discrete is acceptable for all markers.</p></td></tr><tr><td valign="top" width="3%"><p>24</p></td><td valign="top" width="17%"><p>Master warning</p></td><td valign="top" width="14%"><p>Discrete</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>–</p></td><td valign="top" width="10%"><p>–</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>25</p></td><td valign="top" width="17%"><p>NAV 1 and 2 frequency selection</p></td><td valign="top" width="14%"><p>Full range</p></td><td valign="top" width="8%"><p>4</p></td><td valign="top" width="15%"><p>As installed</p></td><td valign="top" width="10%"><p>–</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>26</p></td><td valign="top" width="17%"><p>DME 1 and 2 distance</p></td><td valign="top" width="14%"><p>0-200 NM</p></td><td valign="top" width="8%"><p>4</p></td><td valign="top" width="15%"><p>As installed</p></td><td valign="top" width="10%"><p>–</p></td><td valign="top" width="29%"><p>Recording of latitude and longitude from INS or other navigation system is a preferred alternative.</p></td></tr><tr><td valign="top" width="3%"><p>27</p></td><td valign="top" width="17%"><p>Landing gear squat switch status</p></td><td valign="top" width="14%"><p>Discrete</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>–</p></td><td valign="top" width="10%"><p>–</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>28</p></td><td valign="top" width="17%"><p>Ground proximity warning system (GPWS)</p></td><td valign="top" width="14%"><p>Discrete</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>–</p></td><td valign="top" width="10%"><p>–</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>29</p></td><td valign="top" width="17%"><p>Angle of attack</p></td><td valign="top" width="14%"><p>Full range</p></td><td valign="top" width="8%"><p>0.5</p></td><td valign="top" width="15%"><p>As installed</p></td><td valign="top" width="10%"><p>0.3 % of full range</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>30</p></td><td valign="top" width="17%"><p>Hydraulics</p></td><td valign="top" width="14%"><p>Discrete(s)</p></td><td valign="top" width="8%"><p>2</p></td><td valign="top" width="15%"><p>–</p></td><td valign="top" width="10%"><p>–</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>31</p></td><td valign="top" width="17%"><p>Navigation data</p></td><td valign="top" width="14%"><p>As installed</p></td><td valign="top" width="8%"><p>1</p></td><td valign="top" width="15%"><p>As installed</p></td><td valign="top" width="10%"><p>–</p></td><td valign="top" width="29%"></td></tr><tr><td valign="top" width="3%"><p>32</p></td><td valign="top" width="17%"><p>Landing gear or gear selector position</p></td><td valign="top" width="14%"><p>Discrete</p></td><td valign="top" width="8%"><p>4</p></td><td valign="top" width="15%"><p>As installed</p></td><td valign="top" width="10%"><p>–</p></td><td valign="top" width="29%"></td></tr></table> \* The number in the left hand column reflects the serial number depicted in EUROCAE Document ED-112.
##### AMC5 CAT.IDE.A.190 Flight data recorder *ED Decision 2015/007/R* **PERFORMANCE SPECIFICATIONS FOR THE PARAMETERS TO BE RECORDED FOR AEROPLANES FIRST ISSUED WITH AN INDIVIDUAL COFA UP TO AND INCLUDING 31 MARCH 1998** ***Table 1: Flight data recorder*** <table bgcolor="#d9d9d9" cellpadding="7" cellspacing="0"> <col/> <col/> <col/> <col/> <col/> <col/> <col/> <thead> <tr> <td bgcolor="#808080"><p align="center"> <b>No</b></p> </td> <td bgcolor="#808080"><p align="center"> <b>Parameter</b></p> </td> <td bgcolor="#808080"><p align="center"> <b>Range</b></p> </td> <td bgcolor="#808080"><p align="center"> <b>Sampling interval in seconds</b></p> </td> <td bgcolor="#808080"><p align="center"> <b>Accuracy limits (sensor input compared to FDR readout)</b></p> </td> <td bgcolor="#808080"><p align="center"> <b>Recommended resolution in readout</b></p> </td> <td bgcolor="#808080"><p align="center"> <b>Remarks</b></p> </td> </tr> </thead> <tbody> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Time or relative time count</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 24 hours</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 4</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±0.125 % per hour</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1 second</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Coordinated universal time (UTC) preferred where available, otherwise elapsed time</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Pressure altitude</p> </td> <td bgcolor="#d9d9d9"><p align="left"> -1 000 ft to maximum certificated altitude of aircraft +5 000 ft</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±100 ft to ±700 ft</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 5 ft</p> </td> <td bgcolor="#d9d9d9"><p align="left"> For altitude record error see EASA ETSO-C124a</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 3</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Indicated airspeed or calibrated airspeed</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 50 kt to max V<sub>S0</sub></p> <p align="left">Max V<sub>S0 </sub>to 1.2 V<sub>D</sub></p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±5 %</p> <p align="left">±3 %</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1 kt</p> </td> <td bgcolor="#d9d9d9"><p align="left"> V<sub>S0</sub> stalling speed or minimum steady flight speed in the landing configuration V<sub>D </sub>design diving speed</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 4</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Heading</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 360 degrees</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±2 degrees</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 0.5 degrees</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 5</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Normal acceleration</p> </td> <td bgcolor="#d9d9d9"><p align="left"> -3 g to +6 g</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 0.125 ±</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±1 % of maximum range excluding a datum error of ±5 %</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 0.004 g</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 6</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Pitch attitude</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±75 degrees</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±2 degrees</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 0.5 degrees</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 7</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Roll attitude</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±180 degrees </p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±2 degrees </p> </td> <td bgcolor="#d9d9d9"><p align="left"> 0.5 degrees</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 8</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Manual radio transmission keying</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Discrete</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> -</p> </td> <td bgcolor="#d9d9d9"><p align="left"> -</p> </td> <td bgcolor="#d9d9d9"><p align="left"> On-off (one discrete). An FDR/CVR time synchronisation signal complying with 4.2.1 of EUROCAE ED-55 is considered to be an acceptable alternative means of compliance.</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 9</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Power on each engine</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Full range</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Each engine each second</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±2 %</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 0.2 % of full range</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Sufficient parameters e.g. EPR/N, or Torque/N<sub>P</sub> as appropriate to the particular engine should be recorded to determine power.</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 10</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Trailing edge flap or flight crew compartment control selection</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Full range or each discrete position</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±5 % or as pilot’s indicator</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 0.5 % of full range</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 11</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Leading edge flap or flight crew compartment control selection</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Full range or each discrete position</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> <td bgcolor="#d9d9d9"><p align="left"> -</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 0.5 % of full range</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 12</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Thrust reverser position</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Stowed, in transit and reverse</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Each reverser each second</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±2 % unless higher accuracy uniquely required</p> </td> <td bgcolor="#d9d9d9"><p align="left"> -</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 13</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Ground spoiler and/or speed brake selection</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Full range or each discrete position</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±2 degrees</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 0.2 % of full range</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 14</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Outside air temperatures or total air temperature</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Sensor range</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> <td bgcolor="#d9d9d9"><p align="left"> -</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 0.3ºC</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 15a</p> <p align="left"> <br/> </p> <p align="left">15b</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Autopilot engagement status</p> <p align="left">Autopilot operating modes, auto-throttle and AFCS systems engagement status and operating modes</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> <br/> </p> <p align="left">A suitable combination of discretes</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> <br/> </p> <p align="left">1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> <br/> </p> <p align="left">-</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 16</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Longitudinal acceleration</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ± 1 g</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 0.25</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±1.5 % of maximum range excluding a datum error of ±5 %</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 0.004 g</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 17</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Lateral acceleration</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±1 g</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 0.25</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±1.5 % of maximum range excluding a datum error of ±5 %</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 0.004 g</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 18</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Primary flight controls, control surface positions and/or pilot input (pitch, roll, yaw)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Full range</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±2 degrees unless higher accuracy uniquely required</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 0.2 % of full range</p> </td> <td bgcolor="#d9d9d9"><p align="left"> For aeroplanes with conventional control systems, ‘or’ applies.</p> <p align="left"> For aeroplanes with non-mechanical control systems, ‘and’ applies.</p> <p align="left">For aeroplanes with split surfaces, a suitable combination of inputs is acceptable in lieu of recording each surface separately.</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 19</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Pitch trim position</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Full range</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±3 % unless higher accuracy uniquely required</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 0.3 % of full range</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 20</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Radio altitude</p> </td> <td bgcolor="#d9d9d9"><p align="left"> -20 ft to +2 500 ft</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±2 ft or ±3 % whichever is greater below 500 ft and ±5 % above 500 ft</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1 ft below 500 ft, 1 ft +5 % of full range above 500 ft</p> </td> <td bgcolor="#d9d9d9"><p align="left"> As installed. Accuracy limits are recommended</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 21</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Glide path deviation</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Signal range</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±3 %</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 0.3 % of full range</p> </td> <td bgcolor="#d9d9d9"><p align="left"> As installed. Accuracy limits are recommended</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 22</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Localiser deviation</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Signal range</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> ±3 %</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 0.3 % of full range</p> </td> <td bgcolor="#d9d9d9"><p align="left"> As installed. Accuracy limits are recommended.</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 23</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Marker beacon passage</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Discrete</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> –</p> </td> <td bgcolor="#d9d9d9"><p align="left"> –</p> </td> <td bgcolor="#d9d9d9"><p align="left"> A single discrete is acceptable for all markers.</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 24</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Master warning</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Discrete</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> –</p> </td> <td bgcolor="#d9d9d9"><p align="left"> –</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 25</p> </td> <td bgcolor="#d9d9d9"><p align="left"> NAV 1 and 2 frequency selection</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Full range</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 4</p> </td> <td bgcolor="#d9d9d9"><p align="left"> As installed</p> </td> <td bgcolor="#d9d9d9"><p align="left"> –</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 26</p> </td> <td bgcolor="#d9d9d9"><p align="left"> DME 1 and 2 distance</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 0-200 NM</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 4</p> </td> <td bgcolor="#d9d9d9"><p align="left"> As installed</p> </td> <td bgcolor="#d9d9d9"><p align="left"> –</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Recording of latitude and longitude from INS or other navigation system is a preferred alternative.</p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 27</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Landing gear squat switch status</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Discrete</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> –</p> </td> <td bgcolor="#d9d9d9"><p align="left"> –</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 28</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Ground proximity warning system (GPWS)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Discrete</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> –</p> </td> <td bgcolor="#d9d9d9"><p align="left"> –</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 29</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Angle of attack</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Full range</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 0.5</p> </td> <td bgcolor="#d9d9d9"><p align="left"> As installed</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 0.3 % of full range</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 30</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Hydraulics</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Discrete(s)</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 2</p> </td> <td bgcolor="#d9d9d9"><p align="left"> –</p> </td> <td bgcolor="#d9d9d9"><p align="left"> –</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 31</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Navigation data</p> </td> <td bgcolor="#d9d9d9"><p align="left"> As installed</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 1</p> </td> <td bgcolor="#d9d9d9"><p align="left"> As installed</p> </td> <td bgcolor="#d9d9d9"><p align="left"> –</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> </tr> <tr valign="top"> <td bgcolor="#d9d9d9"><p align="left"> 32</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Landing gear or gear selector position</p> </td> <td bgcolor="#d9d9d9"><p align="left"> Discrete</p> </td> <td bgcolor="#d9d9d9"><p align="left"> 4</p> </td> <td bgcolor="#d9d9d9"><p align="left"> As installed</p> </td> <td bgcolor="#d9d9d9"><p align="left"> –</p> </td> <td bgcolor="#d9d9d9"><p align="left"> <br/> </p> </td> </tr> </tbody> </table> \* The number in the left hand column reflects the serial number depicted in EUROCAE Document ED-112.